Issued Patents All Time
Showing 1–11 of 11 patents
| Patent # | Title | Co-Inventors | Date |
|---|---|---|---|
| 8473254 | Methods for configuring aircraft to meet performance goals and shock wave disturbance constraints | John M. Morgenstern, James B. Bach | 2013-06-25 |
| 7475848 | Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance | John M. Morgenstern | 2009-01-13 |
| 7416155 | Canard position and dihedral for boom reduction and pitch/directional control | Robert S. Cuccias, John M. Morgenstern, Howard Lee | 2008-08-26 |
| 7311287 | Methods for incorporating area ruled surfaces in a supersonic aircraft | John M. Morgenstern, Garret Moose | 2007-12-25 |
| 7216830 | Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction | Brian Quayle, John M. Morgenstern | 2007-05-15 |
| 7070146 | Aircraft thickness/camber control device for low sonic boom | John M. Morgenstern | 2006-07-04 |
| 6942178 | Mach weighted area ruling for supersonic vehicles | John M. Morgenstern | 2005-09-13 |
| 6935592 | Aircraft lift device for low sonic boom | John M. Morgenstern | 2005-08-30 |
| 6921045 | Supersonic aircraft with channel relief control | Ming-Huang Chang, Victor Meza, John M. Morgenstern | 2005-07-26 |
| 6854687 | Nacelle integration with reflexed wing for sonic boom reduction | John M. Morgenstern, Joshua P. Barbieri | 2005-02-15 |
| 6824092 | Aircraft tail configuration for sonic boom reduction | Walter Franklin, John M. Morgenstern, Howard Lee, Brian Quayle, Ken Hajic +1 more | 2004-11-30 |